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ContentsB737-200 Adv Study Notes by Anton Jordaan. |
All of the information, photographs & schematics from this website and much more is now available in a 374 page printed book or in electronic format. *** Updated 05 Aug 2023 *** |
Optimum alt OPTIMUM OPTIMUM 1 ENG INOP HOLDING ALT HOLDING ALT MCT ISA +10 LRC M.74 M.78 220 KIAS 1 ENG INOP A/ICE OFF52T 315 310 290 FL 250 FL 100 FL 118 50T 325 320 300 FL 250 FL 100 FL 130 48T 335 330 305 FL 250 FL 110 FL 145 46T 340 335 315 FL 250 FL 120 FL 160 44T 350 345 325 FL 300 FL 150 FL 174 42T 360 355 335 FL 300 FL 150 FL 188 40T 370 365 345 FL 300 FL 150 FL 204
BUFFET LIMITS
FULL DRAG STALL ![]() @ Stall onset, recover : Go-around thrust, lower nose to 5° @ Go-around thrust, pull up to stick shaker until original altitude Level off and accelerate @ Vref , Flaps 15 @ +ive climb, Gear up, speed 210 @ 150 kts, Flaps 5 @ 180 kts, Flaps 1 @ 190 kts, Flaps up @ 210 kts, MCT, speed 250 @ 250 kts, Level Change, speed 250 Fuel correction for deviation from LRC TANKER ANALYSIS optimum altitude: @ FL 350 CONSTANT TRIP DIST SURPLUS LRC MACH NM BURNOFF± 2,000 1% 2% 800 9% - 4,000 2% 4% 700 8% - 8,000 8% 12% 600 7% -12,000 15% 22% 500 6% Cruise N1 N1 = (2 x Alt/1000) + 10 eg @ FL350 N1 = 70+10 = 80%
WIND-ALTITUDE TRADE
LONG RANGE CRUISE
Eg @ FL290, 50T present wind = -20 kts. Breakeven wind @ FL 330 = {–20 + (1-12)} = -31kts. If HWC is stronger than 31 kts @ FL330, remain @ FL290.
M0.72-M0.74 CRUISE
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